The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.
The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.
Patent No.:
Date of Patent:
Oct. 25, 2011
Filed:
Jun. 25, 2008
Hua Xia, Altamont, NY (US);
Norman Arnold Turnquist, Sloansville, NY (US);
David SO Keung Chan, Niskayuna, NY (US);
Danian Zheng, Simpsonville, SC (US);
Kevin Thomas Mccarthy, Troy, NY (US);
Richard Joseph Gawrelski, Amsterdam, NY (US);
Matthew Damian Pietrzykowski, Clifton Park, NY (US);
Alexander Seth Ross, Albany, NY (US);
Yun LI, Niskayuna, NY (US);
Juntao Wu, Schenectady, NY (US);
Hua Xia, Altamont, NY (US);
Norman Arnold Turnquist, Sloansville, NY (US);
David So Keung Chan, Niskayuna, NY (US);
Danian Zheng, Simpsonville, SC (US);
Kevin Thomas McCarthy, Troy, NY (US);
Richard Joseph Gawrelski, Amsterdam, NY (US);
Matthew Damian Pietrzykowski, Clifton Park, NY (US);
Alexander Seth Ross, Albany, NY (US);
Yun Li, Niskayuna, NY (US);
Juntao Wu, Schenectady, NY (US);
General Electric Company, Niskayuna, NY (US);
Abstract
A fiberoptic multi-parameter sensing system for monitoring turbomachinery system shaft static and dynamic torques, vibration modes and associated operation status includes a multi-furcated fiber bundle based optical splitter configured to transmit light to a surface of at least one turbomachinery system shaft through a plurality of optical fiber bundles disposed at a plurality of locations in proximity to the surface of the at least one shaft, in which the plurality of locations together are arranged in a substantially axial direction between the ends of the at least one shaft. The system further includes an array of high-temperature bifurcated fiber bundle based reflectance probes to receive reflectance signals from the shaft surface and send to an array of photosensitive detectors, configured to detect dynamic light reflected from the at least one turbomachinery system shaft surface in response to the transmitted light during rotation of at least one turbomachinery system shaft and generate dynamic reflected light signals there from. A sensing mechanism is configured to determine a torque or vibration on at least one turbomachinery system shaft in response to the dynamic reflected light signal signatures based on time-domain and frequency-domain signal processes.